EP1682758A1 - Systeme d'alimentation auxiliaire pour moteur hybride - Google Patents

Systeme d'alimentation auxiliaire pour moteur hybride

Info

Publication number
EP1682758A1
EP1682758A1 EP04796461A EP04796461A EP1682758A1 EP 1682758 A1 EP1682758 A1 EP 1682758A1 EP 04796461 A EP04796461 A EP 04796461A EP 04796461 A EP04796461 A EP 04796461A EP 1682758 A1 EP1682758 A1 EP 1682758A1
Authority
EP
European Patent Office
Prior art keywords
power
generator
engine
supplying
gearbox
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP04796461A
Other languages
German (de)
English (en)
Other versions
EP1682758B1 (fr
Inventor
Timothy M. Morris
Wayne R. Spock
Peter Gerald Smith
Matthew J. Schryver
Ronald S. Walther
Robert L. Gukeisen
Edward T. Hagaman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of EP1682758A1 publication Critical patent/EP1682758A1/fr
Application granted granted Critical
Publication of EP1682758B1 publication Critical patent/EP1682758B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16Control of working fluid flow
    • F02C9/18Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
    • F02C6/04Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32Arrangement, mounting, or driving, of auxiliaries
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
EP04796461A 2003-10-27 2004-10-26 Systeme d'alimentation auxiliaire pour moteur hybride Not-in-force EP1682758B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/694,645 US7975465B2 (en) 2003-10-27 2003-10-27 Hybrid engine accessory power system
PCT/US2004/035489 WO2005045215A1 (fr) 2003-10-27 2004-10-26 Systeme d'alimentation auxiliaire pour moteur hybride

Publications (2)

Publication Number Publication Date
EP1682758A1 true EP1682758A1 (fr) 2006-07-26
EP1682758B1 EP1682758B1 (fr) 2010-12-15

Family

ID=34573206

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04796461A Not-in-force EP1682758B1 (fr) 2003-10-27 2004-10-26 Systeme d'alimentation auxiliaire pour moteur hybride

Country Status (9)

Country Link
US (2) US7975465B2 (fr)
EP (1) EP1682758B1 (fr)
JP (1) JP4664304B2 (fr)
CN (1) CN100507239C (fr)
AT (1) ATE491876T1 (fr)
DE (1) DE602004030611D1 (fr)
RU (1) RU2352800C2 (fr)
UA (1) UA91184C2 (fr)
WO (1) WO2005045215A1 (fr)

Families Citing this family (85)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7246482B2 (en) * 2004-07-16 2007-07-24 Honeywell International, Inc. Gas turbine engine bleed air power assist system and method
US7811050B2 (en) * 2006-12-28 2010-10-12 General Electric Company Operating line control of a compression system with flow recirculation
FR2912782B1 (fr) * 2007-02-19 2009-05-22 Snecma Sa Procede de prelevement d'energie auxiliaire sur un turboreacteur d'avion et turboreacteur equipe pour mettre en oeuvre un tel procede
DE102007013345B4 (de) * 2007-03-20 2022-07-07 Airbus Operations Gmbh Energieregelvorrichtung für ein Flugzeug
US8213136B2 (en) * 2007-08-16 2012-07-03 Pratt & Whitney Canada Corp. Engine having power bus fault short circuit control with a disconnection switch
US9719428B2 (en) * 2007-11-30 2017-08-01 United Technologies Corporation Gas turbine engine with pylon mounted accessory drive
FR2928696B1 (fr) * 2008-03-14 2013-09-27 Hispano Suiza Sa Assemblage pour l'entrainement d'accessoires d'une turbine a gaz
ES2358650B1 (es) * 2008-05-30 2012-03-23 Airbus Operations, S.L. Configuración de la instalación neum�?tica en la zona de cola de un avión.
DE102008031185A1 (de) * 2008-07-03 2010-01-07 Rolls-Royce Deutschland Ltd & Co Kg Turbofantriebwerk mit mindestens einer Vorrichtung zum Antreiben mindestens eines Generators
US20100005657A1 (en) * 2008-07-10 2010-01-14 Van Vactor David R Methods and systems to facilitate over-speed protection
US8224552B2 (en) * 2008-07-10 2012-07-17 General Electric Company Methods and systems to facilitate over-speed protection
US8321119B2 (en) * 2008-07-10 2012-11-27 General Electric Company Methods and systems to facilitate over-speed protection
FR2934321B1 (fr) * 2008-07-25 2013-09-27 Hispano Suiza Sa Regulation du debit de carburant preleve dans un circuit carburant d'un aeronef propulse par un moteur.
ES2363897B1 (es) * 2008-10-24 2012-07-04 Airbus Operations, S.L. Unidad de potencia auxiliar (apu) de una aeronave
FR2941743B1 (fr) * 2009-02-05 2011-03-04 Microturbo Demarreur a air pour turbomachine.
WO2010132439A1 (fr) 2009-05-12 2010-11-18 Icr Turbine Engine Corporation Système de stockage et de conversion d'énergie de turbine à gaz
GB0912340D0 (en) * 2009-07-16 2009-08-26 Rolls Royce Plc Aircraft power management system
FR2948151B1 (fr) * 2009-07-17 2011-11-25 Snecma Procede et systeme pour la commande d'un demarreur-generateur de moteur d'aeronef
US9175605B2 (en) * 2009-12-29 2015-11-03 Rolls-Royce Corporation Gas turbine engine surge margin bleed power recuperation
US8794902B1 (en) * 2010-01-26 2014-08-05 II Daniel K. Van Ness System and method to improve the exhaust pressure across a RAM air turbine through secondary flow mixing
US8866334B2 (en) 2010-03-02 2014-10-21 Icr Turbine Engine Corporation Dispatchable power from a renewable energy facility
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
US8672637B2 (en) * 2010-08-17 2014-03-18 Hamilton Sundstrand Corporation Air turbine starter turbine blade airfoil
US8672638B2 (en) * 2010-08-17 2014-03-18 Hamilton Sundstrand Corporation Air turbine starter
US9028208B2 (en) * 2010-08-17 2015-05-12 Hamilton Sundstrand Corporation Air turbine starter turbine nozzle airfoil
FR2964087B1 (fr) * 2010-08-25 2013-06-14 Turbomeca Procede d'optimisation de l'operabilite de motorisation d'un aeronef et groupe de puissance autonome de mise en oeuvre
CA2813680A1 (fr) 2010-09-03 2012-03-08 Icr Turbine Engine Corporation Configurations de moteur a turbine a gaz
US8395275B2 (en) 2010-11-09 2013-03-12 Hamilton Sundstrand Corporation Integrated permanent magnet alternator and cooling fan
US9035802B2 (en) * 2010-12-22 2015-05-19 Textron Innovations Inc. Power safety instrument system
DE102011013746A1 (de) * 2011-03-12 2012-09-13 Man Truck & Bus Ag Über Nebentrieb verbundener Hybridantrieb
EP2696057B1 (fr) 2011-04-07 2017-10-18 Kawasaki Jukogyo Kabushiki Kaisha Moteur d'aéronef
DE102011101197B4 (de) * 2011-05-11 2021-01-28 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbine mit hydraulischem oder pneumatischem Zusatzaggregatantrieb
FR2975547B1 (fr) * 2011-05-20 2013-06-07 Turbomeca Procede de rationalisation de chaine de composants electriques d'un aeronef, architecture de mise en oeuvre et aeronef correspondant
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
US9926849B2 (en) * 2011-06-14 2018-03-27 Honeywell International Inc. Transverse mounted accessory gearbox
US9068515B2 (en) * 2011-12-07 2015-06-30 United Technologies Corporation Accessory gearbox with tower shaft removal capability
US9097186B2 (en) 2012-01-29 2015-08-04 United Technologies Corporation Bevel gear arrangement for axial accessory gearbox
US9206775B2 (en) 2012-02-01 2015-12-08 United Technologies Corporation Fuel preheating using electric pump
EP2870351B1 (fr) * 2012-07-05 2018-04-25 United Technologies Corporation Préchauffage de carburant utilisant une pompe électrique
US9382010B2 (en) * 2012-07-12 2016-07-05 Pratt & Whitney Canada Corp. Aircraft power outtake management
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
CN103661922B (zh) * 2012-08-31 2016-08-31 北京精密机电控制设备研究所 一种伺服机构用电燃气混合动力装置
FR2997467B1 (fr) * 2012-10-26 2016-07-29 Hispano Suiza Sa Boite d'engrenages de prise de mouvement sur une turbomachine, composee de carter assemble
US9045996B2 (en) 2012-11-20 2015-06-02 Honeywell International Inc. Gas turbine engine optimization by electric power transfer
US9500133B2 (en) 2012-12-23 2016-11-22 United Technologies Corporation Mount with an axial upstream linkage for connecting a gearbox to a turbine engine case
US9777639B2 (en) 2012-12-23 2017-10-03 United Technologies Corporation Turbine engine gearbox mount with multiple fuse joints
WO2014143187A1 (fr) 2013-03-15 2014-09-18 Michael Armstrong Gestion de la limite d'optimisation des performances et de prédiction de la durée de vie pour moteur à turbine
FR3007462B1 (fr) * 2013-06-21 2017-11-24 Hispano-Suiza Boitier d'accessoires de turbomachine equipe d'une pompe centrifuge
FR3011882B1 (fr) * 2013-10-11 2018-01-26 Hispano Suiza Sa Boitier d'entrainement d'accessoires pour turbomachine
EP2887536B1 (fr) 2013-12-23 2019-02-27 Rolls-Royce Corporation Système de commande pour un moteur/générateur à double redondance et moteur
US9771932B2 (en) * 2014-02-14 2017-09-26 The Boeing Company Apparatus, controller and method for controlling the cool down of an aircraft engine rotor
US9458770B2 (en) 2014-04-01 2016-10-04 Honeywell International Inc. Optimized engine control using secondary power system horsepower extraction information
FR3026452B1 (fr) * 2014-09-30 2016-10-28 Hispano Suiza Sa Reducteur de vitesse a deux lignes intermediaires de transmission
GB201420444D0 (en) * 2014-11-18 2014-12-31 Rolls Royce Plc A method of starting a gas turbine engine
CN105298685A (zh) * 2014-12-23 2016-02-03 丁义存 涡扇式汽车发动机
CN104608933B (zh) * 2015-01-26 2017-09-15 哈尔滨飞机工业集团有限责任公司 一种发动机惯性分离器控制系统及其控制方法
US20160230843A1 (en) * 2015-02-09 2016-08-11 United Technologies Corporation Gearbox for gas turbine engine
US20170044989A1 (en) * 2015-08-14 2017-02-16 General Electric Company Gas turbine engine stall margin management
US10711702B2 (en) 2015-08-18 2020-07-14 General Electric Company Mixed flow turbocore
US10578028B2 (en) 2015-08-18 2020-03-03 General Electric Company Compressor bleed auxiliary turbine
FR3041379B1 (fr) * 2015-09-18 2017-09-15 Snecma Turbopropulseur d'aeronef
US20170175646A1 (en) * 2015-12-22 2017-06-22 General Electric Company Method and system for stall margin modulation as a function of engine health
US10836505B2 (en) 2016-06-23 2020-11-17 Raytheon Technologies Corporation Operating auxiliary power unit during off-nominal propulsion system operation
US11073085B2 (en) * 2016-11-08 2021-07-27 Raytheon Technologies Corporation Intercooled cooling air heat exchanger arrangement
FR3063782B1 (fr) * 2017-03-07 2021-06-18 Safran Aircraft Engines Procede et dispositif de detection de conditions propices a l'apparition d'un pompage en vue de proteger un compresseur d'une turbomachine d'aeronef
US10502142B2 (en) * 2017-04-11 2019-12-10 United Technologies Corporation Turbine engine gearbox assembly with sets of inline gears
US10762726B2 (en) 2017-06-13 2020-09-01 General Electric Company Hybrid-electric propulsion system for an aircraft
DE102017211117A1 (de) * 2017-06-30 2019-01-03 Siemens Aktiengesellschaft Triebwerkseinrichtung und Verfahren zur Bereitstellung von Antriebsleistung für eine elektrische Einrichtung zur Bereitstellung von elektrischer Energie
US11333076B2 (en) 2017-12-21 2022-05-17 Raytheon Technologies Corporation Power takeoff transmission
CN108104949B (zh) * 2017-12-28 2019-07-02 中科合肥微小型燃气轮机研究院有限责任公司 一种微型燃气轮机多功能减速传动机匣结构
US10479525B2 (en) 2018-04-03 2019-11-19 Kidde Technologies, Inc. Utilization of engine bleed air to provide extended duration emergency aircraft power
FR3081150B1 (fr) * 2018-05-18 2020-06-12 Safran Helicopter Engines Architecture de puissance d'un aeronef
US11332256B2 (en) 2018-08-21 2022-05-17 General Electric Company Fault tolerant hybrid electric propulsion system for an aerial vehicle
US11015480B2 (en) 2018-08-21 2021-05-25 General Electric Company Feed forward load sensing for hybrid electric systems
US11097849B2 (en) 2018-09-10 2021-08-24 General Electric Company Aircraft having an aft engine
US20200086998A1 (en) * 2018-09-13 2020-03-19 Hamilton Sundstrand Corporation Two-turbine environmental control system
US11015532B2 (en) 2018-10-18 2021-05-25 Rolls-Royce North American Technologies, Inc. Parallel starter/generator and air turbine starter
US11261795B2 (en) 2018-10-18 2022-03-01 Rolls-Royce North American Technologies, Inc. Dual mode starter generator
EP3693571B1 (fr) * 2019-02-05 2022-11-02 Raytheon Technologies Corporation Commande de fonctionnement transitoire d'un moteur à turbine à gaz hybride
US11333077B2 (en) * 2019-05-06 2022-05-17 The Boeing Company Systems and methods for transferring mechanical power in a turbine engine
CN110273758B (zh) * 2019-06-04 2020-12-08 湖南航翔燃气轮机有限公司 微型燃气轮机发电机组
US11428171B2 (en) 2019-12-06 2022-08-30 General Electric Company Electric machine assistance for multi-spool turbomachine operation and control
US11713719B2 (en) * 2020-05-07 2023-08-01 The Boeing Company Engine bleed power recovery systems and related methods
CN113217195A (zh) * 2021-06-28 2021-08-06 中科航星科技有限公司 一种航空发动机燃油系统
RU209929U1 (ru) * 2021-11-24 2022-03-23 Публичное Акционерное Общество "Одк-Сатурн" Вспомогательный газотурбинный двигатель с функцией вспомогательной силовой установки

Family Cites Families (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3006145A (en) * 1959-10-14 1961-10-31 Gen Motors Corp Antisurge control using compressor bleed
US3514945A (en) * 1968-10-04 1970-06-02 Avco Corp Gas turbine accessory power drive unit
GB1443333A (en) * 1972-08-12 1976-07-21 Mtu Muenchen Gmbh Aircraft having apparatus for augmenting the lift of the aircraft
US4051472A (en) * 1974-04-08 1977-09-27 International Telephone And Telegraph Corporation Large area motion sensor using pseudo-random coding technique
US4041696A (en) * 1976-05-24 1977-08-16 General Motors Corporation Vehicle turbine manual control
US4184154A (en) * 1976-06-21 1980-01-15 International Telephone And Telegraph Corporation Range and angle determining Doppler radar
US4175701A (en) * 1978-05-15 1979-11-27 The Garrett Corporation Aircraft spraying system and method
DE2946371C2 (de) 1979-11-16 1982-07-08 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Hilfsantriebsanlage für Flugzeughilfsgeräte
US4277787A (en) * 1979-12-20 1981-07-07 General Electric Company Charge transfer device phased array beamsteering and multibeam beamformer
GB2074654A (en) 1980-04-16 1981-11-04 Rolls Royce Remote power system for aircraft
CA1212746A (fr) * 1983-01-31 1986-10-14 R. Ian Macdonald Dephaseur commute optoelectroniquement pour antennes radar et antennes reseau a commande de phase pour signaux transmis par satellite
US4814773A (en) * 1983-05-11 1989-03-21 Hughes Aircraft Company Fiber optic feed network for radar
US4725844A (en) * 1985-06-27 1988-02-16 Trw Inc. Fiber optical discrete phase modulation system
US4885589A (en) * 1988-09-14 1989-12-05 General Electric Company Optical distribution of transmitter signals and antenna returns in a phased array radar system
US5117633A (en) * 1990-07-10 1992-06-02 Allied-Signal Inc. Pneumohydraulic actuator
US5137230A (en) * 1991-06-04 1992-08-11 General Electric Company Aircraft gas turbine engine bleed air energy recovery apparatus
JP2989428B2 (ja) * 1993-06-17 1999-12-13 本田技研工業株式会社 時分割型fmレーダシステム
JP3425570B2 (ja) * 1993-07-02 2003-07-14 独立行政法人航空宇宙技術研究所 ガスタービンエンジン用補機類の駆動方法及びその装置
GB9313905D0 (en) * 1993-07-06 1993-08-25 Rolls Royce Plc Shaft power transfer in gas turbine engines
US5414992A (en) * 1993-08-06 1995-05-16 United Technologies Corporation Aircraft cooling method
WO1995017607A1 (fr) * 1993-12-23 1995-06-29 United Technologies Corporation Detection de saute de regime irrecuperable et d'extinction dans des turbo-moteurs
US5447283A (en) * 1994-02-02 1995-09-05 Grumman Aerospace Corporation Blown boundary layer control system for a jet aircraft
DE19617952C2 (de) * 1996-05-04 1998-07-02 Daimler Benz Aerospace Airbus Absauggeneratorsystem eines Flugzeuges für die Laminarhaltung der Grenzschicht
US5709103A (en) * 1996-08-15 1998-01-20 Mcdonnell Douglas Coporation Electrically powered differential air-cycle air conditioning machine
US6164902A (en) 1998-12-11 2000-12-26 United Technologies Corporation Controlling stall margin in a gas turbine engine during acceleration
JP2001107750A (ja) * 1999-10-05 2001-04-17 Honda Motor Co Ltd 航空機用ガスタービン・エンジンの制御装置
JP3720662B2 (ja) * 2000-01-19 2005-11-30 三菱電機株式会社 車載用レーダ装置
US6663044B1 (en) * 2001-09-20 2003-12-16 Hamilton Sundstrand Corporation Vapor compression cycle environmental control system
US7246482B2 (en) * 2004-07-16 2007-07-24 Honeywell International, Inc. Gas turbine engine bleed air power assist system and method

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2005045215A1 *

Also Published As

Publication number Publication date
CN100507239C (zh) 2009-07-01
US8800918B2 (en) 2014-08-12
EP1682758B1 (fr) 2010-12-15
RU2352800C2 (ru) 2009-04-20
RU2006117061A (ru) 2007-12-10
UA91184C2 (ru) 2010-07-12
JP2007510091A (ja) 2007-04-19
US7975465B2 (en) 2011-07-12
JP4664304B2 (ja) 2011-04-06
US20050103931A1 (en) 2005-05-19
US20090271086A1 (en) 2009-10-29
WO2005045215A1 (fr) 2005-05-19
CN1902389A (zh) 2007-01-24
DE602004030611D1 (de) 2011-01-27
ATE491876T1 (de) 2011-01-15

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